Nested article by additive manufacturing with non-removable internal supporting structure

Patent metadata

Field	Value
Publication number	US-10865990-B2
Application number	US-201715816314-A
Country	US
Kind code	B2
Filing date	Nov 17, 2017
Priority date	Nov 18, 2016
Publication date	Dec 15, 2020
Grant date	Dec 15, 2020

Abstract

An additive manufactured article for a gas turbine having a body with two lateral surfaces elongated in a first direction; at least a nested duct housed within the lateral surfaces and elongated in the first direction; a structure so that the nested duct is structurally connected to an attachment within the lateral surfaces, wherein at least the body, the duct and the structure are manufactured by an additive manufacturing process and the structure includes an array of ribs attached to the duct in order to compensate differential elongation along the first direction of the duct with respect to the attachment of the ribs by flexural deformation.

First claim

The invention claimed is:

1. A fuel injector device for a gas turbine, the fuel injector device comprising:
a body having two lateral surfaces extending along a longitudinal direction and a crosswise direction; the body being streamlined for use in a fluid flow and the lateral surfaces joined to one another at an upstream side form a leading edge of the body and the lateral surfaces joined to one another at a downstream side to form a trailing edge of the body;
a shell defining a gas fuel plenum, the shell nested within the lateral surfaces, wherein the shell is configured to provide a gas fuel flow into the fluid flow;
an oil fuel duct, the oil fuel duct elongated in the longitudinal direction, the oil fuel duct nested within the shell, wherein the oil fuel duct is configured to provide an oil fuel flow into the fluid flow;
an array of ribs extending between the shell and the oil fuel duct, wherein the array of ribs are configured to compensate differential elongation of the nested oil fuel duct with respect to the shell along the crosswise direction by flexural deformation;
struts supported within the lateral surfaces for supporting the shell; and
a cut defined between the struts and a wall structure, the wall structure delimiting a cooling air plenum,
wherein the body, the shell and the oil fuel duct are additively manufactured.

2. The fuel injector device according to claim 1 , wherein each rib of the array of ribs is thicker close to the oil fuel duct and the shell.

3. The fuel injector device according to claim 2 , wherein each rib of the array of ribs is filleted to the oil fuel duct and/or the shell along a parabolic or elliptic profile.

4. The fuel injector device according to claim 1 , wherein an aspect ratio of the each rib of the array of ribs is at least 30.

5. The fuel injector device according to claim 1 , comprising:
a cooling air plenum within the lateral surfaces and upstream of the oil fuel duct and the shell, the cooling air plenum being defined by a wall structure.

6. The fuel injector device according to claim 5 , comprising:
a carrier air plenum defined within the lateral surfaces by the shell and the wall structure.

7. A gas turbine engine comprising:
a combustor; and
the fuel injector device according to claim 1 .

8. The fuel injector device according to claim 1 ,
wherein the struts are substantially parallel with respect to a transverse direction of the fuel injector device.

9. The fuel injector device according to claim 1 , wherein each rib of the array of ribs is wavy.

10. The fuel injector device according to claim 1 , wherein the struts are inclined with respect to a transverse direction of the fuel injector device.

Assignees

• Ansaldo Energia Switzerland AG

Inventors

• Stytsenko Alexey
• Mylnikov Sergey
• Baibuzenko Igor
• Maurer Michael

Classifications

• B22F10/47

  characterised by structural features · CPC title

• B22F10/28

  Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM] · CPC title

• F23R3/28 Primary

  characterised by the fuel supply (burners F23D) · CPC title

• F23R3/16

  with devices inside the flame tube or the combustion chamber to influence the air or gas flow · CPC title

• F02C7/22 Primary

  Fuel supply systems · CPC title